JPH0353445B2 - - Google Patents

Info

Publication number
JPH0353445B2
JPH0353445B2 JP17385784A JP17385784A JPH0353445B2 JP H0353445 B2 JPH0353445 B2 JP H0353445B2 JP 17385784 A JP17385784 A JP 17385784A JP 17385784 A JP17385784 A JP 17385784A JP H0353445 B2 JPH0353445 B2 JP H0353445B2
Authority
JP
Japan
Prior art keywords
turbine
turning device
rotor
journal bearing
rotor wheel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP17385784A
Other languages
Japanese (ja)
Other versions
JPS6153409A (en
Inventor
Sadajiro Takahashi
Juji Sekine
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fuji Electric Co Ltd
Original Assignee
Fuji Electric Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fuji Electric Co Ltd filed Critical Fuji Electric Co Ltd
Priority to JP17385784A priority Critical patent/JPS6153409A/en
Publication of JPS6153409A publication Critical patent/JPS6153409A/en
Publication of JPH0353445B2 publication Critical patent/JPH0353445B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/34Turning or inching gear
    • F01D25/36Turning or inching gear using electric motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

【発明の詳細な説明】 〔発明の属する技術分野〕 この発明は蒸気タービンのターニング装置に関
する。
DETAILED DESCRIPTION OF THE INVENTION [Technical field to which the invention pertains] This invention relates to a turning device for a steam turbine.

〔従来技術とその問題点〕[Prior art and its problems]

蒸気タービンは、運転時においては均一な高温
状態にあるが、運転停止後完全冷却に至るまでの
自然冷却過程において、タービン上、下の温度不
均一により、ロータの曲り現象が起こる。
A steam turbine is in a uniform high temperature state during operation, but during the natural cooling process until complete cooling after shutdown, the rotor bends due to uneven temperatures above and below the turbine.

一般にタービンは、完全冷却に至る途中で再起
動可能なことが要求されるので、このロータ曲り
を防止するため、停止後に低速ターニングができ
るようになつている。低速ターニングの方法とし
ては電動式、油圧キツク式などがあるが、いずれ
もターニング装置本体は、タービンロータに設け
られたホイールとギヤ列を介して連結されてい
る。そしてこのホイールの位置は構造上、ジヤー
ナル軸受の外側すなわち軸端側に置かれるのが普
通である。これを第2図で説明する。1はタービ
ン、2はタービンロータで、前部軸受台3のジヤ
ーナル軸受4と後部軸受台5のジヤーナル軸受6
により軸支されており、7はロータの軸端であ
る。8は前部グランドパツキン、9は後部グラン
ドパツキンである。ターニング装置本体10は後
部軸受台5の上部に設置され、ギヤ列11を介し
てロータホイール12につながつている。この場
合ロータホイールは後部ジヤナール軸受12と軸
端7の間にあるので軸端オーバハング量は長くな
り、それに伴つて付加重量も増すことになる。こ
れはシングルフレキシブルロータにおいて2次危
険速度を低下させ、さらに軸端のアンバランス応
答感度を高めるのでロータ振動に対し不利となつ
ている。そのためにロータホイール位置を後部グ
ランドパツキン9と後部ジヤーナル軸受6との間
に配置しようとすると、ターニング装置本体10
も移動させてタービン1に近づけなければなら
ず、ターニング装置10と図示せぬタービンケー
シングの排気部が干渉するという問題があつた。
In general, turbines are required to be able to be restarted on the way to complete cooling, so in order to prevent rotor bending, low-speed turning can be performed after stopping. Low-speed turning methods include an electric type and a hydraulic type, but in both of these methods, the turning device main body is connected to a wheel provided on a turbine rotor via a gear train. Due to the structure, this wheel is normally placed outside the journal bearing, that is, on the shaft end side. This will be explained with reference to FIG. 1 is a turbine; 2 is a turbine rotor; a journal bearing 4 on a front bearing pedestal 3 and a journal bearing 6 on a rear bearing pedestal 5;
7 is the shaft end of the rotor. 8 is a front gland packing, and 9 is a rear gland packing. The turning device main body 10 is installed on the upper part of the rear bearing stand 5 and is connected to a rotor wheel 12 via a gear train 11. In this case, since the rotor wheel is located between the rear journal bearing 12 and the shaft end 7, the amount of overhang at the shaft end becomes longer, and the additional weight increases accordingly. This reduces the secondary critical speed in a single flexible rotor and further increases the sensitivity of the unbalance response at the shaft end, which is disadvantageous to rotor vibration. Therefore, when trying to arrange the rotor wheel between the rear gland packing 9 and the rear journal bearing 6, the turning device main body 10
The turning device 10 had to be moved closer to the turbine 1, and there was a problem that the turning device 10 interfered with the exhaust part of the turbine casing (not shown).

〔発明の目的〕[Purpose of the invention]

この考案は上述の事情に鑑み、ターニング装置
本体は従来位置に据置いてタービンケーシングの
排気部との干渉がないようにし、かつローターホ
イール位置をグランドパツキンとジヤーナル軸受
との間に配置することにより軸端7側のオーバハ
ング量を短く、付加重量を軽減するようにするこ
とを目的とする。
In view of the above-mentioned circumstances, this idea was developed by leaving the turning device in the conventional position to avoid interference with the exhaust section of the turbine casing, and by locating the rotor wheel between the gland packing and the journal bearing. The purpose is to shorten the amount of overhang on the end 7 side and reduce the added weight.

〔発明の要点〕[Key points of the invention]

この発明は上記目的をターニング装置本体とロ
ータホイールの間に介在するギヤ列のギヤ軸を長
くしてターニング装置本体は従来位置のままでロ
ータホイールをグランドパツキンとジヤーナル軸
受との間に配置することにより達成される。
The object of the present invention is to lengthen the gear shaft of the gear train interposed between the turning device main body and the rotor wheel so that the rotor wheel is placed between the gland packing and the journal bearing while the turning device main body remains in its conventional position. This is achieved by

〔発明の実施例〕[Embodiments of the invention]

第1図はこの発明の実施例を示すもので、第2
図と異なる点はターニング用ロータホイール6を
タービンの後部グランドパツキン9と後部ジヤー
ナル軸受12との間に配設し、ターニング装置本
体をタービン側に近づけないようにギヤ列11の
ギヤ軸11aを従来より長くした点である。これ
により軸端オーバハング量は短かくなり、かつ付
加重量も軽減し、ロータの危険速度、振動に対し
極めて有利となる。
FIG. 1 shows an embodiment of this invention, and FIG.
The difference from the figure is that the turning rotor wheel 6 is disposed between the rear gland packing 9 of the turbine and the rear journal bearing 12, and the gear shaft 11a of the gear train 11 is changed from the conventional one to prevent the turning device body from approaching the turbine side. The point is that it is longer. This reduces the amount of overhang at the shaft end, reduces additional weight, and is extremely advantageous against critical speeds and vibrations of the rotor.

本実施例はターニング装置後部配置を示してい
るが、前記配置の場合にも、後部配置と対称配置
すれば同じように実施可能である。
Although this embodiment shows a rear arrangement of the turning device, the above arrangement can also be implemented in the same way if the arrangement is symmetrical to the rear arrangement.

〔発明の効果〕〔Effect of the invention〕

この発明によればロータホイールをグランドパ
ツキンとジヤーナル軸受との間に設けたので軸端
におけるオーバハング量は短縮され、かつ付加重
量も軽減し、ロータの危険速度、振動に対して極
極めて有利になつた。またギヤ軸を長くしてター
ニング装置本体をタービンに近づけないようした
ので、タービンの排気部に干渉されることがな
い。
According to this invention, since the rotor wheel is provided between the gland packing and the journal bearing, the amount of overhang at the end of the shaft is shortened, and the additional weight is also reduced, which is extremely advantageous against critical speeds and vibrations of the rotor. Ta. Furthermore, since the gear shaft is made long to keep the turning device body away from the turbine, it will not be interfered with by the exhaust section of the turbine.

【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの発明の一実施例であるターニング
装置とタービンとの関係位置を示す概略構成図、
第2図は従来技術によるターニング装置とタービ
ンとの関係位置を示す概略構成図である。 2:タービンロータ、4:前部ジヤーナル軸
受、5:後部ジヤーナル軸受、8,9:グランド
パツキン、10:ターニング装置本体、11:ギ
ヤ列、12:ロータホイール。
FIG. 1 is a schematic configuration diagram showing the relative position of a turning device and a turbine according to an embodiment of the present invention;
FIG. 2 is a schematic diagram showing the relative position of a turning device and a turbine according to the prior art. 2: Turbine rotor, 4: Front journal bearing, 5: Rear journal bearing, 8, 9: Gland packing, 10: Turning device main body, 11: Gear train, 12: Rotor wheel.

Claims (1)

【特許請求の範囲】[Claims] 1 ジヤーナル軸受で軸支されたタービンロータ
ーにターニング用ロータホイールを取付け、この
ロータホイールにギヤ列を介して連結されるター
ニング装置において、このロータホイールがジヤ
ーナル軸受とタービンのグランドパツキン部との
間に設けられていることを特徴とする蒸気タービ
ンのターニング装置。
1. In a turning device in which a turning rotor wheel is attached to a turbine rotor supported by a journal bearing and connected to this rotor wheel via a gear train, this rotor wheel is connected between the journal bearing and the gland packing part of the turbine. A turning device for a steam turbine, comprising: a turning device for a steam turbine;
JP17385784A 1984-08-21 1984-08-21 Turning device for steam turbine Granted JPS6153409A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17385784A JPS6153409A (en) 1984-08-21 1984-08-21 Turning device for steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17385784A JPS6153409A (en) 1984-08-21 1984-08-21 Turning device for steam turbine

Publications (2)

Publication Number Publication Date
JPS6153409A JPS6153409A (en) 1986-03-17
JPH0353445B2 true JPH0353445B2 (en) 1991-08-15

Family

ID=15968427

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17385784A Granted JPS6153409A (en) 1984-08-21 1984-08-21 Turning device for steam turbine

Country Status (1)

Country Link
JP (1) JPS6153409A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH667285A5 (en) * 1986-02-14 1988-09-30 Sulzer Ag ROLLER WITH A HARD COVERED SURFACE.
CN105840249B (en) * 2016-04-19 2017-05-17 哈尔滨汽轮机厂有限责任公司 Installing method of magnetic resistance type probe used for measuring rotating speed of turning gear of steam turbine

Also Published As

Publication number Publication date
JPS6153409A (en) 1986-03-17

Similar Documents

Publication Publication Date Title
JPH0417762Y2 (en)
JP3620167B2 (en) Reheat axial flow steam turbine
JPH0353445B2 (en)
JP2004116317A (en) Rotor balance adjustment method for turbocharger with rotating electric machine
JPS5993515A (en) Bearing device for turbo-charger
JPS5852099B2 (en) Balance weight of rotating body
JPS5918207A (en) Clearance adjusting device of steam turbine
JPS6238525B2 (en)
JP3431219B2 (en) Spindle device of machine tool
JP2000183436A5 (en) Gas laser device containing halogen gas
GB1189440A (en) Overspeed Brake for Rotative Engines
JPS6376913A (en) Doubel thrust bearing with journal bearing
JP2875028B2 (en) Turbo type fluid machine
JP2768789B2 (en) Gas turbine rotor
GB2011553A (en) Turbomachine casings
JPS599311A (en) Fixing device of skirt ring for bearing in water wheel generator
JPS588821A (en) Rotating machine bearing support device
JPH081360Y2 (en) Bearing device
CN119765714A (en) Integrated design of auxiliary exciter and exciter rotor and bearing cover
JPS6044557B2 (en) Thrust bearing cooling control device
KR100754480B1 (en) Bearing housing for turbomachinery
JPS6022780Y2 (en) Shaft runout adjustment device for vertical shaft rotating electric machines
JPS6012601U (en) Shaft stabilizer
DOLEZAL et al. Design philosophy for bearing supports of present-day turbine engine rotors
JPH08303476A (en) Rotary main shaft